1-24 of 95 Books
Wind-tunnel investigation of aerodynamic loading on a 0.237-scale model of a remotely piloted research vehicle with a thick, high-aspect-ratio supercritical wing
Wind-tunnel investigation of aerodynamic loading on a 0.237-scale model of a remotely piloted research vehicle with a thick, high-aspect-ratio supercritical wing
By Thomas A. Byrdsong
High-area-ratio rocket nozzle at high combustion chamber pressure--experimental and analytical validation
High-area-ratio rocket nozzle at high combustion chamber pressure--experimental and analytical validation
By Robert S. Jankovsky
A modified T-value method for selection of strain gages for measuring loads on a low aspect ratio wing
A modified T-value method for selection of strain gages for measuring loads on a low aspect ratio wing
By Ming Han Tang
F-18 High Alpha Research Vehicle surface pressures
F-18 High Alpha Research Vehicle surface pressures
By David F. Fisher
Wind-tunnel investigation of aerodynamic loading on a 0.237-scale model of a remotely piloted research vehicle with a thick, high-aspect-ratio supercritical wing
Wind-tunnel investigation of aerodynamic loading on a 0.237-scale model of a remotely piloted research vehicle with a thick, high-aspect-ratio supercritical wing
By Thomas A Byrdsong
In-flight investigation of shuttle tile pressure orifice installations
In-flight investigation of shuttle tile pressure orifice installations
By Timothy R. Moes
Comparison of wing-span averaging effects on lift, rolling moment, and bending moment for two span load distributions and for two turbulence representations
Comparison of wing-span averaging effects on lift, rolling moment, and bending moment for two span load distributions and for two turbulence representations
By Jacob H. Lichtenstein
A summary of the forebody high-angle-of-attack aerodynamics research on the F-18 and the X-29A aircraft
A summary of the forebody high-angle-of-attack aerodynamics research on the F-18 and the X-29A aircraft
By Lisa J. Bjarke
Comparison of wing-span averaging effects on lift, rolling moment, and bending moment for two span load distributions and for two turbulence representations
Comparison of wing-span averaging effects on lift, rolling moment, and bending moment for two span load distributions and for two turbulence representations
By Jacob H Lichtenstein
Effects of flow separation and cove leakage on pressure and heat-transfer distributions along a wing-cove-elevon configuration at Mach 6.9
Effects of flow separation and cove leakage on pressure and heat-transfer distributions along a wing-cove-elevon configuration at Mach 6.9
By William D. Deveikis
Design of a 4-1/2 stage turbine with a stage loading factor of 4.66 and high specific work output
Design of a 4-1/2 stage turbine with a stage loading factor of 4.66 and high specific work output
By P. F. Webster
Fluctuating loads measured on an over-the-wing supersonic jet model
Fluctuating loads measured on an over-the-wing supersonic jet model
By Conrad M. Willis
Experimental performance and analysis of 15.04-centimeter-tip-diameter, radial-inflow turbine with work factor of 1.126 and thick blading
Experimental performance and analysis of 15.04-centimeter-tip-diameter, radial-inflow turbine with work factor of 1.126 and thick blading
By Kerry L. McLallin
Effect of an alternate winglet on the pressure and spanwise load distributions of a first-generation jet transport wing
Effect of an alternate winglet on the pressure and spanwise load distributions of a first-generation jet transport wing
By Lawrence C. Montoya
Aircraft dynamic loads due to flow separation
Aircraft dynamic loads due to flow separation
By North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development.
The pressure distribution at zero lift on a slender delta wing at transonic speeds
The pressure distribution at zero lift on a slender delta wing at transonic speeds
By Michael Charles Peter Firmin
The use of load frequency distributions in the specification of design requirements for commercial aircraft
The use of load frequency distributions in the specification of design requirements for commercial aircraft
By O. Buxbaum
A method for the prediction of wing response to nonstationary buffet loads =
A method for the prediction of wing response to nonstationary buffet loads =
By B. H. K. Lee
Two-dimensional normal fences on a flat plate
Two-dimensional normal fences on a flat plate
By C. S. Barnes
Agricultural aircraft flight loads
Agricultural aircraft flight loads
By P. J. Foden
Measurements of drag, base pressure and base aerodynamic heat transfer appropriate to 8.5⁰ semi-angle sharp cones in free flight at mach numbers from 0.8 to 3.8
Measurements of drag, base pressure and base aerodynamic heat transfer appropriate to 8.5⁰ semi-angle sharp cones in free flight at mach numbers from 0.8 to 3.8
By G. H. Greenwood
Measurements of fluctuating pressures in and behind the bomb bay of a Canberra aircraft
Measurements of fluctuating pressures in and behind the bomb bay of a Canberra aircraft
By Colin William Skingle
Theoretical and experimental vibration and buckling results for blunt truncated conical shells with ring-supported edges
Theoretical and experimental vibration and buckling results for blunt truncated conical shells with ring-supported edges
By Sidney C. Dixon